《Chinese Journal of Aeronautics》

作品数：4771被引量：15660H指数：33
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《Chinese Journal of Aeronautics》
主办单位：Chinese Society of Aeronautics and Astronautics & Beihang University
最新期次：2025年3期更多>>
发文主题：BASED_ONAIRCRAFTGUIDEAUTHORSOPTIMIZATION更多>>
发文领域：航空宇航科学技术一般工业技术自动化与计算机技术金属学及工艺更多>>
发文作者：王仲奇张军屈香菊高正红冯国泰更多>>
发文机构：北京航空航天大学西北工业大学南京航空航天大学哈尔滨工业大学更多>>
发文基金：国家自然科学基金中国航空科学基金国家重点基础研究发展计划中国博士后科学基金更多>>
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Flow control mechanism of sprays using dual synthetic jets
《Chinese Journal of Aeronautics》2025年第3期1-17,共17页Wei HE Songjiang FENG Zhenbing LUO Lurui XIA Xiong DENG Sen LI Sheng XU 
supported by the National Natural Science Foundation of China(Nos.U2341202,12402333).
Dual Synthetic Jets (DSJ) can directly affect the development of spray through the complex vortex structure. The mechanism of flow control on spray and its thermal management application are studied by combining exper...
关键词：Dual synthetic jets Fow cantrol Spray cooling Heat pipe Piezoelectric atomizer Heat transfer enhancerment 
Swarm intelligence:A survey of model classification and applications
《Chinese Journal of Aeronautics》2025年第3期163-182,共20页Chao WANG Shuyuan ZHANG Tianhang MA Yuetong XIAO Michael Zhiqiang CHEN Lei WANG 
co-supported by the National Natural Science Foundation of China(No.61873017);the Academic Excellence Foundation of Beihang University for PhD Students,China.
Swarm Intelligence (SI) is a collective behavior that emerges from interaction between individuals in a group. Typical SI includes fish schooling, ant foraging, bird migration, and so on. A great deal of models have b...
关键词：Swarm intelligence Ant colony optimization Self-driven particle models Pheromone communication models Leadership decision models Empirical research models 
A critical review on oxidation behavior of Co-based superalloys
《Chinese Journal of Aeronautics》2025年第3期183-206,共24页Chenghao PEI Qingshuang MA Qiuzhi GAO Yue YANG Yuhang DU Hailian ZHANG Huijun LI 
support from the National Natural Science Foundation of China(Nos.52171107,52201203);the Hebei Provincial Natural Science Foundation,China(No.E2021501026);the National Natural Science Foundation of China-Joint Fund of Iron and Steel Research(No.U1960204).
The novel Co-based superalloys are extensively used in gas-powered and jet engine turbines due to their excellent high-temperature performance, achieved by strengthening the L12-γ′ ordered phase. This review present...
关键词：COBALT SUPERALLOYS OXIDATION Alloying elements MICROSTRUCTURE Temperature 
Scaling analysis and experimental validation for incident shock wave/boundary layer interactions under the influence of gradual expansion waves
《Chinese Journal of Aeronautics》2025年第3期207-221,共15页Yunjie GUO Ziyun WANG Huijun TAN Yue ZHANG Yufeng HUANG Hongchao XUE Hang YU Hao ZHANG 
Cowl-induced incident Shock Wave/Boundary Layer Interactions (SWBLI) under the influence of gradual expansion waves are frequently observed in supersonic inlets. However, the analysis and prediction of interaction len...
关键词：Supersonic flow Shock wave/boundary layer interactions Boundary layer separation Scaling analysis Prediction of interaction length 
Effect of ion solvation energy on electrohydrodynamic behavior of ionic liquid droplets in electrospray thrusters
《Chinese Journal of Aeronautics》2025年第3期222-233,共12页Yipeng FAN Chong CHEN Huifeng KANG Guangqing XIA Chang LU Yajie HAN 
supported by the National Key R&D Program of China(No.2020YFC2201100);the National Natural Science Foundation of China(Nos.12175032,12102082,12275044,12402327,12405290 and 12211530449);the Joint Program of the Science and Technology Program of Liaoning,China(No.2023JH2/101700285);the Fundamental Research Funds for the Central Universities of China(Nos.DUT22RC(3)078,DUT23RC(3)040 and DUT24ZD106);the S&T Program of Hebei,China(No.246Z2301G);the S&T Innovation Program of Hebei,China(Nos.SJMYF2022X18 and SJMYF2022X06);the Beijing Engineering Research Center of Efficient and Green Aerospace Propulsion Technology and Advanced Space Propulsion Laboratory of BICE,China(No.LabASP-2023-07).
The electrospray thruster supplied by ionic liquid is a promising micro-propulsion thruster with small size and precise thrust, which can emit both cations and anions to achieve self-neutralization. In order to furthe...
关键词：Ionic liquid ELECTROSPRAY ELECTROHYDRODYNAMICS Ion solvation energy Ion evaporation 
Denoising graph neural network based on zero-shot learning for Gibbs phenomenon in high-order DG applications
《Chinese Journal of Aeronautics》2025年第3期234-248,共15页Wei AN Jiawen LIU Wenxuan OUYANG Haoyu RU Xuejun LIU Hongqiang LYU 
co-supported by the Aeronautical Science Foundation of China(Nos.2018ZA52002,2019ZA052011).
With the availability of high-performance computing technology and the development of advanced numerical simulation methods, Computational Fluid Dynamics (CFD) is becoming more and more practical and efficient in engi...
关键词：Computational fluid dynamics High-order discon tinuous Galerkin method Gibbs phenomenon Graph neural networks Zero-shot learning 
Soot volume fraction measurements in aero-engine model combustor outlet using two-color laser-induced incandescence
《Chinese Journal of Aeronautics》2025年第3期249-261,共13页Linsen WANG Pengji DING Sijie YAN Jie LI Jingwei Zhang Chaozong WANG Zhibo CAO Quan ZHOU Jinhe MU Gang Meng Wenyan SONG Zhenyu XU Bo Yan Shuang CHEN 
supported by the National Key Research and Development Program of China(No.2020YFA0405700).
Quantitative measurement of Soot Volume Fraction (SVF) is an essential prerequisite for controlling soot particle emissions from aero-engine combustors. As an in-situ and non-intrusive optical diagnostic technique, La...
关键词：Aero-engine combustor Combustion diagnostics Soot Volume Fraction(SVF) Laser-Induced Incandescence(II) Inlet pressure Air preheat temperature 
Variable leading-edge cone method for waverider design
《Chinese Journal of Aeronautics》2025年第3期262-279,共18页Zhihao LI Chongwen JIANG Shuyao HU Chun-Hian LEE 
supported by grants from the National Natural Science Foundation of China(No.U20B2006);the Guangdong Basic and Applied Basic Research Foundation(No.2022A1515110145);Young Elite Scientists Sponsorship Program by China Association for Science and Technology(No.2022QNRC001).
The optimization of the waverider is constrained by the reversely designed leading edge and the constant shock angle distribution. This paper proposes a design method called the variable Leading-Edge Cone (vLEC) metho...
关键词：Hypersonic vehicles Waverider design methods Leading-edge cone method Variable shock angles Direct design method 
Longitudinal combustion instability in a hypergolic liquid bipropellant combustor with single dual-swirl coaxial injector
《Chinese Journal of Aeronautics》2025年第3期280-291,共12页Wei CHU Kangkang GUO Yiheng TONG Yongjie REN Boqi XU Wansheng NIE 
support from the National Natural Science Foundation of China(No.12002386).
Self-excited longitudinal combustion instabilities were investigated in a hypergolic liquid bipropellant combustor, which applied single dual-swirl coaxial injector. Hot-fire tests were conducted for four different in...
关键词：Longitudinal combustion instability Dual-swirl coaxial injector Unsymmetrical Dimethylhydrazine/Nitrogen Tetroxide(UDMH/NTO) Photomultiplier Tubes(PMT) Spray fluctuation Pressure wave Modulation 
Aerodynamic analysis of rotor-to-rotor interactions in different octocopter configurations
《Chinese Journal of Aeronautics》2025年第3期292-315,共24页Aqib AZIZ Yongjie SHI Yang LIU Guohua XU 
supported by the National Natural Science Foundation of China(No.11972190).
Rotor-to-rotor interaction among neighboring rotors of a multirotor has great significance for aerodynamically efficient multirotor design. Current research is conducted to analyze aerodynamic performance of different...
关键词：Rotor-to-rotor interaction Virtual blade method Octocopter configurations Aerodynamically efficient HOVER Forward f1ight 
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